Periodic and quasi-periodic orbit design based on the center manifold theory-Reference-Cited by-同舟云学术

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Periodic and quasi-periodic orbit design based on the center manifold theory

Published:2019-07 Issue: Volume:160 Page:672-682
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Akiyama Yuki,Bando Mai,Hokamoto Shinji^ORCID

Funder

JSPS KAKENHI

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference35 articles.

1. Lunar communications with libration-point satellites;Farquhar;J. Spacecraft Rockets,1967

2. A halo-orbit lunar station;Farquhar;Astronaut. Aeronaut.,1972

3. Dynamics and Mission Design Near Libration Point Orbits–Volume 1: Fundamentals: the Case of Collinear Libration Points;Gómez,2001

4. Low-Energy Lunar Trajectory Design;Parker,2014

5. Solar System Dynamics;Murray,1999

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Stochastic Trajectory Planning for Autonomous Aerobraking Using Convex Optimization and Covariance Control;Journal of Guidance, Control, and Dynamics;2024-06-05

2. Trajectory Design in Irregular Gravitational Fields Based on Center Manifold Theory;Journal of Guidance, Control, and Dynamics;2023-04-02

3. A multi-step method to calculate long-term quasi-periodic orbits around the Sun-Earth $L_{1}$/$L_{2}$;Astrophysics and Space Science;2022-10

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